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UNIT I

SATELLITE ORBITS

1. State Keplers first law.

It states that the path followed by the satellite around the primary will be

an ellipse. An ellipse has two focal points F1 and F2. The center of mass of the

two body system, termed the barycenter is always centered on one of the foci.

e= a2-b

2

a

2. State Keplers second law.

It states that for equal time intervals, the satellite will sweep out equal

areas in its orbital plane, focused at the barycenter.

3. state Keplers third law.

It states that the square of the periodic time of orbit is perpendicular to

the cube of the mean distance between the two bodies.

a3/n

where, n= Mean motion of the satellite in rad/sec.

= Earths geocentric gravitational constant.

With the n in radians per sec.the orbital period in second is given by,

4. Define apogee and perigee.

The point farthest from the earth is known as apogee.

The point closest from the earth is known as perigee.

5. What is line of apsides?

The line joining the perigee and apogee through the center of the earth is

known as line of apsides.
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It is defined as the angle produced by intersection of local horizontal

plane and the plane passing through the earth station, the satellite and center of

earth.

12. State Newtons second law.

Second law of motion states that the acceleration of the body is directly

proportional to the force acting on it and inversely proportional to the mass.

F=ma

13. Find a range and antenna elevation angle for the satellite parameter

R=6371km; aGso=42164m; b=36.23o.

Solution:

Range, d= R2+a

2GSO-2RaGsocosb

d= (6371)2+(42164)

2-2(6371)(42164)cos(36.23

0)

d=37215km.

Antenna elevation angle,

El=arc cos(

sinb)

El=Cos-1

(

sin (36.230

))

El=480.

14. Write the expressions of nozzle expansion.

From the nozzle expression, the equation can be written as given below.

F=-

Ve+(Pe-Pa)Ae.

Where, Pe=exhaust pressure at the exit plane.

Pa= ambient pressure of the atmosphere.

This equation says that the total thrust of the rocket is compossed of the

momentum thrust and the pressure thrust.

15. Define sub-Satellite point.
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The point on the earth vertically under the satellite is called sub-satellite

point . The height of the terrain above the reference ellipsoid at the sub-satellite

point is denoted by Hss. The height of the satellite above this is denoted by hss.

Thus the total height is,

h= Hss+hss

16. Define sun transit outage.

The sun comes with the beam width of the earth station antenna is known

as sun transit outage. During this period, the sun behaves as extremely noisy

source and it is blanks out all signals from satellite. This effect is known as sun

transit outage.

17. Write short notes on station keeping.

It is the process of maintaining the satellites attitude against differentfactors that can cause drift with time. Satellites need to have their orbits

adjusted from time to time, because, the satellite is initially placed in the correct

orbit. But, natural forces induce a progressive drift.

18. Define specific impulse.

The characteristic that is used to describe the propellant performance is

called specific impulse ISP. It is defined as,

ISP=

.

19. Write short notes on atmospheric Drag.

The atmospheric drag is significant for near earth satellite below or above

1000km. This drag radius the velocity at the perigee because of this the satellite

does not reach the same apogee height on successive revolution. So that the

semi major axis and eccentricity are reduced.

a=a0

)

2/3

20. Define Prograde orbit and Retrograde orbit.

Prograde orbit: An orbit in which the satellite moves in same direction as

the earth rotation. It is also known as the direct orbit.
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Retrograde orbit: An orbit in which the satellite moves in counter to

direction of earth rotation.

UNIT II

SPACE SEGMENT AND SATELLITE LINK DESIGN

1. Write short notes on attitude control system.

It is the system that achieves and maintains the required attitudes. The

main functions off attitude control system include maintaining accurate satellite

position throughout the life span of the system.

2. Describe the spin stabilized satellites.

In a spin stabilized satellites, the body of the satellite spins at about 30 to100 rpm about the axis perpendicular to the orbital plane. The satellites are

normally dual spin satellites with a spinning section and a despun section on

which antennas are mounted. These are kept stationary with respect to earth by

counter rotating the despun section.

3. What are the main functions of a space craft management .

The main functions of a space craft management are given below.

1. To control the orbit and attitude of the satellite.

2. To monitor the status of all the sensors in the satellite.

3. To switch on/off some sections in communication system.

4. Write short notes on telemetry.

The telemetry system is present in the satellite, this subsystem collects

data from many/all sensors present in the satellite and retransmit it into the earth

station.

5. Write short notes on tracking.

Tracking is nothing but to find the position of the satellite in space.

Tracking is very important during the transfer orbit and drift phase of the

satellite launch. We know that lots of disturbing forces may change the attitude
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and orbit of a satellite, so it is necessary to track the satellite and send correction

signals.

6. Write the equations of Link-Power Budget.

The power output of the link is power at the receiver the major source of

loss in any ground satellite link is the free space spreading loss.

[LOSSES]=[FSL]+[RFL]+[AML]+[AA]+[PL]

Where, FSL=Free Space Spreading Loss(dB)

RFL=Receiver Feeder Loss(dB)

AML=Antenna Misalignment Loss(sB)

AA= Atmospheric Absorption(dB)

PL= Polarization mismatch Law(dB)

7. What is an EIRP?

EIRP means Equivalent Isotropic Radiated Power. It is a measure of

radiated or transmitted power of an antenna.

8. What is an intermodulation noise?

Intermodulation distortion in high power amplifier can result in signalproduct which appear as noise and it is referred to as Intermodulation noise.

9. What is an system noise?

Noise temperature is very important concept in receivers. By using this,

thermal noise which is generated by active and passive devices in the receiver

can be calculated.

The noise power is given by,

Pn=KTnB

Where, Pn=Noise power

K=Boltzmans constant

Tn=Noise temperature of source(in Kelvin)

B=Bandwidth in Hz
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10. What is an antenna loss?

It is added to noise received as radiation and the total antenna noise

temperature is the sum of the equivalent noise temperature of all these sources.

11. Define sky noise.

It is a term used to describe the microwave radiation which is present

throughout universe and which appears to originate from matter in any form, atfinite temperature.

12. Define noise factor.

An alternative way of representing amplifier noise is by means of its

noise factor. In defining the NF of an amplifiers, usually taken as 290K.

13. Define saturation flux density.

The flux density required at the receiving antenna to produce saturation

of TWTA is termed the saturation flux density.

14. Define Satellite uplink.

The link through which the earth station transmits the signal and the

satellite receive the same is known as uplink. [C/No] equation in the last title

carrier to noise ratio can be applied to uplink.

[

]u= [EIRP]u+[

]-[L]u-[K]

Here, the subscript u is used to denote the uplink.

[C/No] ratio appears at satellite receiver.

[EIRP]u=Earth station EIRP.

[G/T]u= satellite receiver G/T

15. Define satellite downlink.

The link through which the satellite transmit the signal and the earth

station receive it,

Subscript D is used to indicate the downlink in the following equation.

[

]

D= [EIRP]

D+[

]

D-[L]

D-[K].

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16. Define Carrier to Noise Ratio.

The performance of satellite line is measured by carrier to noise ratio, it is

given as CNR or C/N.

C/N in db is given as [C/N]

[

] =[PR]-[PN]

[C/N0]= [EIRP]+[G/T]-[L]-[K] dB. Hz.

17. A transponder require a saturation flux density of -110 d Bw/m2, operating

frequency of 14 GHz. Total loss =200dB Find [EIRP].

Solution:

Here, [s]=-110dB

F=14GHz

[L]=200dB

[A]=-(21.45+20logf)=-44.37

[EIRP] =[ s]+[A]+[L]

[EIRP]=-110-44.37+200

[EIRP]=45.63 dB.

18. What is noise weighting?

The method used to improve the post detection signal to noise ratio is

referred to as noise weighting.

19. Write short notes on body stabilization.

The body stabilization is also known as three axis satellite. The

stabilization is achieved by controlling the moment of the satellite along the 3-

axis. (i.e) yaw,pitch,r oll With respect to the reference.

20. What is meant by Pitch angle?

An angle produced by the movement of a spacecraft about an axis which

is perpendicular to its longitudinal axis is known as Pitch angle.
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UNIT III

SATELLITE ACCESS

1. What are methods of multiple access techniques?

Two methods of multiple access techniques are given below.

FDMA (Frequency division multiple access techniques)

TDMA(Time division multiple access techniques)

2. What is CDMA? And its types?

In this method, each signal is associated with a particular code that is

used to spread the signal in frequency and time. Its types are:

Spread spectrum multiple access.

Pulse address multiple access.

3. What is an TDMA? What are the advantages?

Only one carrier uses the transponder at any one time, and therefore

intermodulation products, which results from the non-linear amplification of

multiple carriers are absent.

Advantages: The transponder traveling wave tube can be operated at maximum

power output.

4. Define multiple access.

Various earth stations may transmit more number of carriers. At that

time, a transponder is loaded with more than one number of carriers. This is

known as multiple access.

5. What is CBR?

An un modulated carrier wave is provided during the first part of the

carrier and bit-timing recover (CBR) time slot. It is used as a synchronizing

signal for local oscillator in the detector circuit. In the remaining part of CBR

time slot, the carrier is modulated by a known phase change sequence.

6. What is BCW?

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The copy of burst code word (BCW) is stored in all the earth stations.

Incoming bits in the burst are compared with the BCW. The receiver detects the

group of received bits matched with BCW. Then, accurate time reference for

the burst position in frame is provided.

7. What is amplitude modulation?

The modulated signal may be expressed as,

am(t)={kas(t)+1}Ac sin(ct+)

For special case where the modulating signal in sine wave with angular

frequency cos and letting k=m,above equation becomes

am(t)=(msinst+1)Ac sinct

where, m=modulation index.

8. What are the analog transmission technique.

The analog transmission techniques are given as,

Amplitude modulation

Frequency division multiplexing.

Frequency modulation.

9. What are the components of encryption?

The symmetric encryption has 5 components. They are,

Plain text

Encryption algorithm

Secret key

Cipher-text

Decryption algorithm.

10.What are the types of vedio signals?

Generally two types of signals are transmitted through the satellite

circuits.

Broadcast equality commercial television.

Television used for business conferencing.
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11. What are the disadvantages of FDMA.

Sensitive to fading

Stabilization is difficult.

Sensitive to random frequency modulation.

Sensitive to inter modulation distortion.

12. Write short notes on voice.

Voice is a telephone speech signals. Generally bandwidth upto 20 Hz.

Telephone handset acts as the acoustic electric transmission. Which converts

voice/sound signal to electrical signal.

13. What are the limitations of FDMA-satellite access?

If the traffic in the downlink is much heavier than that in the

uplink, then FDMA is relatively inefficient. So, bandwidth of theuplink channel is not fully used.

Compared with TDMA, FDMA has less flexibility in reassigning

channels.

Carrier frequency assignments are hardware controlled.

14. distinguish between pre-assigned and demand-assigned TDMA satellite

access.

Preassigned TDMA Demand assigned TDMA

Example for preassigned TDMA is

CSC for the SPADE network. CSCcan accommodate upto 49 earth

stations in the network and 1 reference

station.

In TDMA,reassigning of channels is

more flexible. Different methods areused to provide traffic flexibility.

All bursts are of equal length. Each

burst contains 128 bits. The bit rate is

138kb/s,

The burst length may be kept constant

and the number of bursts per frame

used by the given station is variedwhen the demand is varied.

15. Mention the merits and demerits of TDMA over FDMA.

In TDMA, only one carrier uses the transponder at any time. So,

intermodulation noise is reduced.

16. What is an multiple access technique?
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A transponder to be loaded by a number of carriers. These may originate

from a number of earth stations. This mode of operation known as multiple

access technique.

17. What is meant by space division multiple access?

The satellite as a whole to be accessed by earth stations widely separated

geographically but transmitting on the same frequency i.e. known as frequency

reuse. This method of access known as space division multiple access.

18. What is burst code word and burst position acquisition?

Burst code: It is a binary word, a copy of which is stored at each earth

station.

Burst position acquisition: A station just entering, or reentering after a

long delay to acquire its correct slot position is known as burst position

acquisition.

19. Define guard time.

It is necessary to prevent the bursts from overlapping. The guard time

will vary from burst to burst depending on the accuracy with which the various

bursts can be positioned within each frame.

20. Write short notes on open-loop timing control.

It is a method of transmit timing. In this method, according to burst time

plan, a station transmits at a fixed interval. Necessary guard time is allowed to

absorb the variations in propagation delay.

UNIT IV

EARTH SEGMENT

1. What are the components of Earth station?

The earth station comprises set of equipment, which is used to make a

link with satellite mainly the used components are,

Transmitters

Receivers.
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Antennas

Tracking System.

Terrestrial interface.

Primary power.

Test equipment.

2. Write short notes on MATV.

MATV is a Master Antenna TV System. It is used to provide reception of

DBS TV channels to the user group. It consists of one outdoor unit and various

indoor units. Each user can independently access all the channels. It has a low

signal to noise ratio. The receiver antenna diameter is 2m-3m.

3. Write short notes on CATV.

CATV is a Community Antenna TV system. As in MATV system, it

consists of one outdoor unit and separate feeds for each sense of polarization.

The channels are then combined by using combiner block. The combined

signal is a multiplexed signal which is transmitted through the cable to the

users. The signal is retransmitted from a low power VHF TV transmitter.

4. Define Y-factor.

Y-factor is the ratio of output noise measured when the receiver is

connected to a hot noise to the output noise measured when connected to thecold source(Tc).

The receiver excess noise Te is related to the Y-factor by

Tw=(Tb-YTc)/(Y-1)

5. Write the expressions of universal antenna.

The universal antenna formula is

and

=

=

If a is atmospheric absorption at zenith then the elevation angle 0 is given

by
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=

sin

Where, A= correction factor.

6. What is an EIRP?



7. Define Carrier to Noise Ratio.

The performance of satellite line is measured by carrier to noise ratio, it is

given as CNR or C/N.

C/N in db is given as [C/N]

[

] =[PR]-[PN]

[C/N0]= [EIRP]+[G/T]-[L]-[K] dB. Hz.

8. What is a monopulse?

If the antenna generates different patterns with nulls on the axis, in

azimuth and elevation planes, then it is called monopulse tracking method. The

monopulse antenna presents a low systematic pointing error or the order of

0.1 . The monopulse technique is more complex and highly expensive.

Hence it is not used popularly.

9. What are the basic requirements of an earth station antenna?.

The basic requirements of an earth station antenna are listed below.

The antenna must have a low noise temperature. The ohmic losses

of antenna must also be maximum.

The antenna must be rotated or steered easily so that a trackingsystem can be employed to point the antenna beam accurately.

The antenna radiation must have a low side lobe level to reduce

interference from unwanted signals and also to minimize

interference into other satellites and terrestrial systems.

The antenna must have a high directive gain.
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10. Write short notes on TVRO.

The TVRO is a Receive Only Home TV systems. TVRO transmission

takes place in Ku- band. Single mesh type reflector may be used which focuses

the signal into a single feed horn, which has 2 separate outputs, one for c-band

signals and other for ku-band signals.

11. What is a tracking?

The tracking is an important operation of the earth station. The efficiency

of earth station depends as to how efficiently it points the antenna beam to the

satellite both in the transmit and receive mode.

12. Write a short notes on step by step technique.

The step by step technique is the most popular technique used for

tracking. In this technique maximum reception of the received signal is needed

and it is performed by moving and checking the beam continuously. This

tracking gives a systematic pointing of the order of 0.203db.

13. A transponder require a saturation flux density of -110 d Bw/m2, operating

frequency of 14 GHz. Total loss =200dB Find [EIRP].

Solution:

Here, [s]=-110dB

F=14GHz

[L]=200dB

[A]=-(21.45+20logf)=-44.37

[EIRP] =[ s]+[A]+[L]

[EIRP]=-110-44.37+200

[EIRP]=45.63 dB.

14. A satellite downlink at 12 GHz operates with a transmit power of 6 W and

an antenna gain of 48.2 dB. Calculate the EIRP in dBW.


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EIRP=10log6+48.2

EIRP=56dBW.

15. What is a transponder?

In a communication satellite, the equipment which provides the

connecting link between the satellitestransmit and receive antennas is referred

to as the transponder.

16. What is meant by input back off of a transponder?

The operating point of TWT must be shifted closer to the linear portion of

the curve to reduce the intermodulation distortion. So, input power is reduced.

This is known as input backoff.

17. What is TWTA?

TWTA means travelling wave tube amplifier. The TWTA is widely used

in transponder to provide the final output power required to the transtube and its

power supplies.

18. Give the formulae to compute the uplink carrier to noise ratio.

Uplink carrier to noise ratio is [C/N0]u

[C/N0]= [EIRP]u+[G/T]u-[L]u-[K]

[Lu]=Losses in dB.

[K]=constant=-228.6

19. What is meant by intermodulation distortion?

When multiple carriers are passed through the device with the non-linear

transfer characteristic, more serious form of distortion is introduced known as

intermodulation distortion.

20. What is polarization interleaving?

Overlap occurs between channels, but these are alternatively polarized

left hand circular and right hand circular to reduce interference to acceptable

levels. This is referred to as polarization interleaving.
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UNIT V

SATELLITE APPLICATIONS

1. Write short notes on INTELSAT.

INTELSAT stands for International Telecommunication Satellite. In

april 6, 1965 first INTELSAT was launched. It is nicknamed as Early Bird.

Initially 11 members are made in present; there are more than 155 members and700 earth station. INTELSAT-6 uses microprocessor with switching process.

These are used for whether, DTH, telex etc.

2. What does INTELSAT,INMARSAT,INSAT stands for.

INTELSAT stands for International Telecommunication Satellite.

INSAT stands for Indian National Satellite system.

INMARSAT stands for International Marine Satellite Organization.

3. What are the satellite mobile services?

The satellite mobile services are

Mobile Satellite Service.(MSAT)

Very Small Aperture Terminal(VSAT)

Direct Broadcast Satellite (DBS) Global Positioning System(GPS)

Microsats

Orbcomm

Iridium.

4. What are VSATs?

VSAT is a Very Small Aperture Terminal System. It provides two waycommunication facilities. Typical user groups include banking and financial

institutions, airline, hotel booking agencies and large retail stores with

geographically dispersed outlets.

5. Write short notes on INMARSAT.

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It stands for International Marine Satellite Organization. It founded in the

year 1979. It provides voice and data service. It is used in marine assessment

for disaster management.

6. What are the INMARSAT services?

The INMARSAT services are

Telephony Telex

Facsimile

E-mail

Slow speed data for marine

Aeronautical

Landmobile

Telephony

7. Define LEO.

LEO stands for Low Earth Orbit. It is defined as orbit within the locus

extending from the earth surface upto an altitude of 2000 km, the commonly

accepted definition for LEO is between 160-200 km above the earth surface.

8. Define MEO.

MEO stands for Medium Earth Orbit. It lies between 8000km and

18000km above the earth surface. MEO satellite ranges for orbital period for

about 2 to 12 hrs. Some MEO orbits are in near perfect circles and therefore

have constant altitude and travel at a constant speed.

9. Define Satellite Navigational System.

Satellite Navigation are SATNAV system is a system of satellite that

provides autonomous geospatial positioning with global coverage. It allowselectronic receivers to determine the latitude, longitude and attitude position

within a few meters using timing signals transmitted from a line of sight by

radio from the satellite.

10. What are the services and features of GSM?

The GSM services are classified into 2.
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Tele services.

Data services.

Features of GSM:

Subscriber Indentity Module (SIM)

On the air privacy.

11. What is a direct broadcasting satellite?

Satellite used for direct broadcasting is called DBS. These Service

include audio, TV,internet services. Satellite and antenna footprint can be made

to cover large area of earth.

12. What are the INSAT services.

The INSAT provides 3 main services

Long distance communication

TV and Radio broadcasting.

Meterology.

13. Write a short notes on digital audio broadcast.

The digital audio broadcasting through satellite is used to provide, high

quality audio signals to the consumers. In early days, it was called as digital

audio broadcast. Now it is commonly termed as

SDARS (Satellite Digital Audio Radio Service)

DARS (digital Audio Radio Service).

14. What are the applications of GPS?

Mobile communication to provide position updates.

Spot beam identification.

Used in ships

Scientists, surveyors, etc.

15. What is ECEF?

The geocentric equatorial coordinate system is used with the GPS system.

It is called as earth centered, earth fixed coordinate system.
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16. What is dilution of precision?

Position calculations involve range differences and where the ranges are

nearly equal; any error is greatly magnified in the difference. This effect,

brought a result of the satellite geometry is known as dilution of precision.

17. What is PDOP?

With the GPS system, dilution of position is taken into account through afactor known as the position dilution of precision.

18. What is a transponder capacity?

DBS television is also known as DTH TV. It needs more channels. So,

audio and video components of a TV program are digitized. So, compression

technique is used. Bandwidth is reduced due to this compression symbol rate

which can be transmitted in a given bandwidth is given by

Rs=BIF/(1+)

= Roll off factor.

19. What is the difference between a geostationary orbit and a geosynchronous

orbit?

In the geostationary orbit, a satellite appears stationary relative to the

earth. The satellite follows the same speed as the earth, so it seems to appear

stationary from the earth.

20. What is the orbital spacing of satellites?

For high power satellites orbital spacing 90. This orbital spacing is

required to avoid adjacent interference.

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